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280 inch solid
Notional solid rocket engine. Study 1963. Operational date would have been February 1973 Used on Nova MM 14B launch vehicle. Solid propellant rocket stage. Operational date would have been February 1973. Nova MM 14B first stage.

AKA: Nova MM 14B-1. Status: Study 1963. Thrust: 46,208.00 kN (10,387,971 lbf). Specific impulse: 265 s. Specific impulse sea level: 238 s. Burn time: 118 s. Height: 52.80 m (173.20 ft). Diameter: 7.10 m (23.20 ft).

Country: USA. Launch Vehicles: Nova MM 14B. Propellants: Solid. Stages: 280 inch solid.



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